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Daisuke Ichihara
Daisuke Ichihara
Other namesD. Ichihara, 市原 大輔
Verified email at mae.nagoya-u.ac.jp
Title
Cited by
Cited by
Year
Ten-ampere-level, applied-field-dominant operation in magnetoplasmadynamic thrusters
D Ichihara, T Uno, H Kataoka, J Jeong, A Iwakawa, A Sasoh
Journal of Propulsion and Power 33 (2), 360-369, 2017
322017
Anode geometry effects on ion beam energy performance in helicon electrostatic thruster
A Uchigashima, T Baba, D Ichihara, A Iwakawa, A Sasoh, T Yamazaki, ...
IEEE Transactions on Plasma Science 44 (3), 306-313, 2016
132016
Electrostatic-magnetic-hybrid thrust generation in central–cathode electrostatic thruster (CC–EST)
A Sasoh, H Kasuga, Y Nakagawa, T Matsuba, D Ichihara, A Iwakawa
Acta Astronautica 152, 137-145, 2018
112018
Electrostatic ion acceleration across a diverging magnetic field
D Ichihara, A Uchigashima, A Iwakawa, A Sasoh
Applied Physics Letters 109 (5), 2016
112016
Electrostatic–magnetic hybrid ion acceleration for high-thrust-density operation
D Ichihara, R Nakano, Y Nakamura, K Kinefuchi, A Sasoh
Journal of Applied Physics 130 (22), 2021
92021
Modelling of a 1 T high-temperature superconducting applied field module for a magnetoplasmadynamic thruster
JR Olatunji, NM Strickland, MRG Winchester, K Kinefuchi, D Ichihara, ...
TENCON 2021-2021 IEEE Region 10 Conference (TENCON), 173-178, 2021
92021
Effects of magnetic field profile near anode on ion acceleration characteristics of a diverging magnetic field electrostatic thruster
D Ichihara, A Iwakawa, A Sasoh
Journal of Applied Physics 122 (4), 2017
82017
Energy conversion efficiency of electrical exploding foil accelerators
D Ichihara, G Fukushima, D Kuwabara, A Sasoh
AIP Advances 11 (9), 2021
52021
Operation characteristics of steady-state, applied field, rectangular magnetoplasmadynamics (MPD) thruster
D Ichihara, S Harada, H Kataoka, S Yokota, A Sasoh
Journal of the Japan Society for Aeronautical and Space Sciences 63 (2), 37-44, 2015
52015
Steady-state, applied-field, rectangular magnetoplasmadynamics thruster using hollow cathode
A Sasoh, D Ichihara, T Enoki, S Yokota
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4276, 2012
52012
Numerical and experimental study on the behavior of vortex rings generated by shock–bubble interaction
K Kitamura, Z Yue, T Fujimoto, H Asai, A Kubota, M Myokan, D Ichihara, ...
Physics of Fluids 34 (4), 2022
32022
Thrust Density Enhancement in an Electrostatic–Magnetic Hybrid Thruster
D Ichihara, K Oka, A Higo, Y Nakamura, K Kinefuchi, A Sasoh
Journal of Propulsion and Power 37 (6), 973-976, 2021
32021
High-specific-impulse electrostatic thruster with argon propellant
D Ichihara, T Matsuba, A Iwakawa, A Sasoh
Journal of Propulsion and Power 36 (2), 256-263, 2020
32020
Central and external cathode operations in a diverging-magnetic-field electrostatic thruster
D Ichihara, Y Nakagawa, A Iwakawa, A Sasoh
Journal of Propulsion and Power 36 (1), 68-77, 2020
32020
Steady-state, applied-field, rectangular MPD thrusters
S Yokota, D Ichihara, H Kataoka, S Harada, A Sasoh
IEPC Paper 246, 2013, 2013
32013
Energetic ion and plasma oscillation measurements during plume mode operation of a hollow cathode
A Suzuki, K Kinefuchi, D Ichihara, S Cho, H Watanabe, K Kubota
Physics of Plasmas 30 (7), 2023
22023
Similar Thrust Performance in Diverging-Magnetic-Field Electrostatic Thruster with Monoatomic Propellants
D Ichihara, A Sasoh
Journal of Propulsion and Power 35 (1), 236-238, 2019
22019
Ten-Ampere-Level, Direct Current Operation of Applied-Field Magnetoplasmadynamics (MPD) Thruster using LaB6 Hollow Cathode
H Kasuga, K Mizutani, D Ichihara, A Iwakawa, A Sasoh, K Kojima, ...
35th International Electric Propulsion Conference, 2017
22017
Power matching between plasma generation and electrostatic acceleration in helicon electrostatic thruster
D Ichihara, Y Nakagawa, A Uchigashima, A Iwakawa, A Sasoh, ...
Acta Astronautica 139, 157-164, 2017
22017
定常作動同軸 AF-MPD の電極形状が推進性能に及ぼす影響
鵜生, 知輝, 片岡, 久志, 鄭栽勲, 市原, 岩川, 輝,佐宗, 章弘
平成 26 年度宇宙輸送シンポジウム: 講演集録= Proceedings of Space …, 2015
22015
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